Author: Rational Advisory Committee for, Aeronautics / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

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1. Ailerons. Flight tests of retractable ailerons on highly tapered wing [with list of references]; by J. W. Wetmore.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:6/714

2. Airfoil theory at supersonic speed [with list of references], by H. Schlichting; [translation by S. Reiss from] Deutsche Luftfahrtforschung, Jahrbuch 1937.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:8/897

3. Fuel-oil. Comparison of ignition characteristics of Diesel fuels as determined in engines and in constant-volume bomb [with list of references]; by Robert F. Selden.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:6/710

4. Ice. Preliminary study of prevention of ice on aircraft by use of engine-exhaust heat [with reference]; by Lewis A. Rodert.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:6/712

5. Spin (aircraft). Approximate spin design criterion for monoplanes [with list of references]; by Oscar Seidman and Charles J. Donlan.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:6/711

6. Strength of materials. Limit of stability of curved plate strip under shear and axial stresses [with list of references]; by A. Kromm, Luftfahrtforschung, v. 15, no. 10-11, Oct. 10, 1938.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June 1939
SuDoc number:: Y 3.N 21/5:8/898

7. Wings. Comparison of several tapered wings designed to avoid tip stalling [with list of references]; by Raymond F. Anderson.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: June, 1939
SuDoc number:: Y 3.N 21/5:6/713

8. Radiators. Drag of airplane radiators with special reference to air heating (comparison of theory and experiment) [with list of references], by B. Göthert; [translation by J. Vanier from] Luftfahrtforshung, v. 15, no. 9, Sept. 10, 1938.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: May 1939
SuDoc number:: Y 3.N 21/5:8/896

9. Air flow in boundary layer of elliptic cylinder [with list of references]; by G. B. Schubauer.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: 1939
SuDoc number:: Y 3.N 21/5:5/652

10. Propellers. Tests of 2 full-scale propellers with different pitch distributions, at blade angles up to 60° [with list of references]; by David Biermann and Edwin P. Hartman.

Corporate/Agency Authors:: Rational Advisory Committee for, Aeronautics
Publisher:: Rational Advisory Committee for, Aeronautics
Date:: 1939
SuDoc number:: Y 3.N 21/5:5/658

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